A standard spacecraft bus compatible with NASA launch vehicles, including STS, for four reference missions (Sun, Earth, stellar pointing from low Earth orbit, Earth pointing from geostationary orbit) was designed. The modular serviceable design stems from its use of passive acme screws for module attachment and scoop proof electrical connectors for electrical interfaces. A flight support system includes command and telemetry links.


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    Titel :

    Multimission Modular Spacecraft (MMS). A Serviceable Design Spacecraft


    Beteiligte:
    E. Falkenhayn (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    4 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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